View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 57128U 26144.65475277 +.00000000 +00000-0 +36504-4 0 00008
2 57128 43.0015 212.2486 0001858 272.3825 87.6814 15.27577109 02
| Epoch (UTC): | 24 May 2026 15:42:50 |
| Eccentricity: | 0.0001858 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 212.2486° |
| argument of perigee: | 272.3825° |
| revolutions per day: | 15.27577109 |
| mean anomaly at epoch: | 87.6814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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